The benefits of the utilization of effluents of the Space Station Environmental Control and Life Support (ECLS) system are examined. Various ECLSS-propulsion system interaction options are evaluated and compared on the basis of weight, volume, and power requirements. Annual propulsive impulse to maintain station altitude during a complete solar cycle of eleven years and the effect on station resupply are considered.


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    Titel :

    Space station propulsion-ECLSS interaction study


    Beteiligte:

    Erscheinungsdatum :

    14.02.1986


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch